EP2148987B1 - Suspension system for a linear compressor - Google Patents

Suspension system for a linear compressor Download PDF

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Publication number
EP2148987B1
EP2148987B1 EP08783091.5A EP08783091A EP2148987B1 EP 2148987 B1 EP2148987 B1 EP 2148987B1 EP 08783091 A EP08783091 A EP 08783091A EP 2148987 B1 EP2148987 B1 EP 2148987B1
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EP
European Patent Office
Prior art keywords
motor
hole
compressor
set forth
compressor assembly
Prior art date
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Active
Application number
EP08783091.5A
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German (de)
English (en)
French (fr)
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EP2148987A1 (en
Inventor
Dietmar Erich Bernhard Lilie
Claudio Roberto Hille
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Whirlpool SA
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Whirlpool SA
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Publication date
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Publication of EP2148987A1 publication Critical patent/EP2148987A1/en
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Publication of EP2148987B1 publication Critical patent/EP2148987B1/en
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B35/00—Piston pumps specially adapted for elastic fluids and characterised by the driving means to their working members, or by combination with, or adaptation to, specific driving engines or motors, not otherwise provided for
    • F04B35/04—Piston pumps specially adapted for elastic fluids and characterised by the driving means to their working members, or by combination with, or adaptation to, specific driving engines or motors, not otherwise provided for the means being electric
    • F04B35/045—Piston pumps specially adapted for elastic fluids and characterised by the driving means to their working members, or by combination with, or adaptation to, specific driving engines or motors, not otherwise provided for the means being electric using solenoids
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B35/00—Piston pumps specially adapted for elastic fluids and characterised by the driving means to their working members, or by combination with, or adaptation to, specific driving engines or motors, not otherwise provided for
    • F04B35/04—Piston pumps specially adapted for elastic fluids and characterised by the driving means to their working members, or by combination with, or adaptation to, specific driving engines or motors, not otherwise provided for the means being electric
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/0027—Pulsation and noise damping means
    • F04B39/0044—Pulsation and noise damping means with vibration damping supports
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/12—Casings; Cylinders; Cylinder heads; Fluid connections
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/12—Casings; Cylinders; Cylinder heads; Fluid connections
    • F04B39/127—Mounting of a cylinder block in a casing

Definitions

  • the present invention refers to a suspension system to be used in reciprocating compressors driven by a linear motor, in which the fixation of the motor-compressor assembly to the shell is generally carried out through spring elements, particularly flat springs.
  • the present solution refers to an improvement in the suspension system for linear compressors of the type described in patent application WO2006/049511 .
  • the gas compression mechanism occurs by the axial movement of a piston in the interior of a cylinder provided with a head, in which are positioned the suction and discharge valves which regulate the gas inlet and gas outlet in relation to the cylinder.
  • the piston is driven by an actuator, which carries a magnetic component driven by a linear motor.
  • the piston is connected to a resonant spring and the piston, jointly with the magnetic component and the spring, form the resonant assembly of the compressor.
  • the compressor is mounted in the interior of a shell which forms a hermetic environment in relation to the exterior thereof and which internally carries a suspension spring assembly, onto which is mounted the compressor.
  • the function of the suspension springs is to minimize the transmission of vibration from the motor-compressor assembly to the shell.
  • the vibrations generated during normal operation of the compressor are produced by oscillation of the mass of the mechanical assembly of the compressor, resulting from the reciprocating movement of the compressor in relation to the motor, said vibrations having a preferential direction and being more accentuated in the movement direction of the piston and less intense in directions orthogonal to this movement direction.
  • the solution disclosed in WO2006/049511 presents a flat spring, made of steel-sheet, with a determined profile that offers low resistance to the movement in the direction of the gas compression, thus transmitting low vibration to the shell.
  • this type of spring also has a determined profile that confers a determined deformation resistance, in the directions orthogonal to the piston movement, which is sufficiently high to support the compressor, with little deformation of the flat springs, due to the gravity force acting on the mechanical assembly of the compressor.
  • the suspension systems with parallel flat springs of the known solutions present a problem related to the great accelerations which occur during handling and transport of the compressors.
  • the relative movement of the mechanical assembly of the compressor in the interior of the shell can be so intense as to cause some parts of said mechanical assembly to impact the inner surface of the shell.
  • Important parts of the compressor can suffer damages during these impacts. Said parts are, for example, the electric motor, the suction chamber, the electrical cables, etc., which may offer risk of accident to the final user, with severe consequences.
  • a suspension system for a linear compressor presenting: a hermetic shell; a motor-compressor assembly suspended, with its axis horizontally disposed, in the interior of the shell and presenting opposite ends spaced from said shell by an axial spacing; mounting elements, each attached to a respective end of the motor-compressor assembly and axially projecting therefrom; suspension springs mounted to the shell and to each respective mounting element.
  • the suspension system comprises stop elements, each having a mounting portion rigidly attached to the shell and a free end portion disposed between a respective end of the motor-compressor assembly and the adjacent suspension spring, and a first distance, defined between the stop element and the adjacent end of the motor-compressor assembly, being smaller than said axial spacing and smaller than a second distance defined between the free end portion of the stop element and an adjacent suspension spring.
  • each stop element is provided with a through hole, by which passes, with a radial gap, an extension of a respective mounting element defined between the adjacent end of the motor-compressor assembly and the free end attached to an adjacent suspension spring.
  • the present invention is mainly applicable to suspension systems using flat springs, preventing them from breaking, but without interfering with their function of dampening the vibrations of the motor-compressor assembly.
  • a reciprocating hermetic compressor which comprises, in the interior de a hermetic shell 1, a motor-compressor assembly 10 suspended in the interior of said shell 1 and presenting opposite ends 10a, 10b spaced from said shell 1.
  • the motor-compressor assembly 10 comprises a cylinder block 11 closed, in one end 11a, by a cylinder cover 12 and defining, in an opposite end lib, a respective end 10b of the motor-compressor assembly 10.
  • Cylinder block 11 defines a compression cylinder 13, inside which a piston 14, driven by the motor of the motor-compressor assembly 10, is axially displaced during operation of the compressor, in suction and discharge cycles of refrigerant gas.
  • the cylinder 13 has an open end, through which the piston 11 is lodged, and an opposite end, closed by a valve plate 15, against which is externally seated the cylinder cover 12.
  • the valve plate 15 carries at least one discharge valve and, optionally, at least one suction valve, which regulate the gas inlet and gas outlet in the interior of the cylinder 13. In the illustrated construction, the valve plate 15 carries a suction valve 15a and a discharge valve 15b.
  • the piston 14 is connected to a resonant spring 16 by a rod 14a, the piston 14 being axially displaced in the interior of the cylinder 13 by an actuator assembly 17 comprising a magnetic component coupled to the rod 14a and axially impelled upon energization of a linear motor 18.
  • the motor-compressor assembly comprises mounting elements 20, each projecting from one of the two opposite ends 10a, 10b of the motor-compressor assembly 10, and suspension springs 30, each mounted to the shell 1 and to a respective mounting element 20.
  • each mounting element 20 is defined by at least one rigid rod 21, 22 attached to the motor-compressor assembly, each rigid rod having a free end 21a, 22a axially projecting from a respective end 10a, 10b of the motor-compressor assembly 10.
  • the motor-compressor assembly 10 incorporates, in a single piece or by fixation, from each of its opposite ends 10a, 10b, at least one mounting element 20.
  • the mounting of the motor-compressor assembly 10 in the interior of the shell 1 occurs through a suspension means comprising two flat suspension springs 30, each presenting a fixation portion 31 and a movable portion 32, extended from the fixation portion 31 and through which it is mounted and affixed to the motor-compressor assembly 10.
  • the fixation portion 31 and movable portion 32 define, in a single piece, a respective flat spring, which is obtained, for example, in the form of a flexible plate, such as a metallic blade, for example, with a reduced thickness in the displacement direction of the piston 14 and presenting a determined flexibility.
  • the flat spring presents its movable portion 32 in the form of a coil, initiating its curvature, in an increasing development, from a central portion 33 of said movable portion 32, through which the flat spring is attached to the motor-compressor assembly 10.
  • the central portion 33 presents at least one hole, for example, a central hole 34, to receive an end 21a, 22a, of a rigid rod 21, 22, for fixation of the motor-compressor assembly 10.
  • the central portion 33 of at least one flat suspension spring 30 further presents a pair of other holes, in the form of eccentric holes 35, for fixation of the cylinder cover 12 to the suspension spring 30.
  • the rigid rod 21 is attached to the cylinder cover 12 through two fixation means, each mounted through an eccentric hole 35 of the suspension spring 30, aligned to a respective blind hole provided in the rigid rod 21 of the cylinder cover 12.
  • This mounting defines, in the motor-compressor assembly 10, two points for supporting the latter to the shell 1, which act together with another support point defined close to the opposite end of said motor-compressor assembly 10, in order to prevent the motor-compressor assembly 10 from rotating around its longitudinal axis, in the interior of the shell 1.
  • the two support points defined close to the cylinder cover 12 of the motor-compressor assembly 10 are laterally provided and equally spaced in relation to the axis of the rigid rod 22 which defines, in the illustrated construction, a single support point close to the opposite end of the motor-compressor assembly 10. It should be understood that multiple support points can be provided between the opposite ends 10a, 10b of the motor-compressor assembly 10 and the suspension springs 30.
  • the mounting element comprises a set of rigid rods that are laterally adjacent and project from the part that carries them.
  • the rigid rod presents two eccentric blind holes parallel to each other, each to be aligned with an eccentric hole of an adjacent suspension spring 30.
  • said rigid rod 21 projects from the cylinder cover 12
  • said rigid rod 21 presents a non-circular cross section, for example, substantially rectangular, having a determined width in one of the vertical or horizontal directions substantially inferior to a length taken in the other of said directions.
  • the width of the rigid rod 21 is taken in the vertical direction, said width being substantially inferior to a length taken in the horizontal direction.
  • the construction of the rigid rod 21 may present, such as illustrated, an oblong profile.
  • the fixation portion 31 of an adjacent suspension spring 30 is provided with two eccentric holes 35 for the passage of fixation means 50 such as, for example, screws, which attach the suspension spring 30 to the cylinder cover 12 of the motor-compressor assembly 10.
  • suspension springs 30 present lateral and transversal flexibility and a sufficiently high rigidity to support the motor-compressor assembly 10 in the interior of the shell 1.
  • the suspension system of the present invention is applied to a motor-compressor assembly 10 mounted in the interior of the shell 1, with its axis horizontally disposed so that the opposite ends 10a, 10b of said motor-compressor assembly 10 are spaced from an adjacent wall portion of the shell 1, by an axial spacing AA, taken according to said longitudinal axis.
  • the present suspension system comprises stop elements 40, each having a mounting portion 41 rigidly attached to the shell 1, and a free end portion 42, provided between a respective and adjacent end 10a, 10b of the motor-compressor assembly 10 and an adjacent suspension spring 30.
  • Each stop element 40 is mounted at a first distance d, in relation to the adjacent end 10a, 10b of the motor-compressor assembly 10, smaller than a second distance D defined between the free end portion 42 of the stop element 40 and an adjacent suspension spring 30.
  • the distance d to mount the stop element 40 in relation to the adjacent end 10a, 10b must be also smaller than the axial spacing AA between each of said end 10a, 10b and the shell 1.
  • the first distance d between each stop element 40 and the adjacent end 10a, 10b of the motor-compressor assembly 10 is calculated in order that, in case an end 10a, 10b of the motor-compressor assembly 10 seats against the adjacent stop element 40, when axially displaced in this direction, said seating occurs before the adjacent mounting elements 20 and suspension spring 30 hit a confronting wall portion of the shell 1 and before the movable portion 32 of the opposite suspension spring 30 reaches the free end portion 42 of the adjacent stop element 40.
  • the first distance d between each opposite end 10a, 10b of the motor-compressor assembly 10 and the free end portion 42 of the adjacent stop element 40 is smaller, not only in relation to the second distance D, but also in relation to the axial spacing AA between each mounting element 20 and a confronting wall portion of the shell 1.
  • each suspension spring 30 is attached to a respective stop element 40, through appropriate fixation means 50, such as screw, rivet, welding, etc., and each stop element 40 is attached to the shell 1 through respective appropriate fixation means, such as welding or gluing.
  • each stop element 40 comprises, adjacent to the respective mounting portion 41, at least one lower projection 40a, generally produced by deformation, to be electrically welded (by projection) to the inner surface of the shell 1.
  • each stop element 40 is defined by an end portion of said stop element 40, opposite to the free end portion 42.
  • the second distance D between the free end portion 42 of the stop element 40 and the movable portion 32 of the adjacent suspension spring 30 is obtained by dimensioning a support portion 44 carried by an adjacent mounting portion 41 of each stop element 40, each of said support portion 44 attaching, through an adequate fixation means 50, such as welding, screw, rivet, etc, the fixation portion 31 of a suspension spring 30.
  • the support portion 44 is preferably conformed to be defined in a parallel or substantially parallel plane and spaced from a plane containing the free end portion 42 of the respective stop element 40, by a value corresponding to the second distance D, taken in the mounting region of a respective suspension spring 30.
  • the support portion 44 is incorporated, in a single piece, to the respective stop element 40, during obtention thereof. It should be understood that the support portion 44 can be defined in a separate piece adequately attached to the stop element 40.
  • the support portion 44 is defined by deforming the piece being conformed.
  • the deformation is in the form of a curvature provided in the mounting portion 41.
  • the free end portion 42 of at least one of the stop elements 40 is positioned in order that the adjacent mounting element 20 is disposed externally to the contour of said free end portion 42.
  • the radial retention of the mounting element 20 is made exclusively by the structure of the adjacent suspension spring 30.
  • each stop element 40 is provided with a through hole 43, through which a respective mounting element 20 is lodged and retained against displacements orthogonal to the axis of the motor-compressor assembly 10.
  • Each mounting element 20 has a portion of its extension, defined between the adjacent end 10a, 10b of the motor-compressor assembly 10 and the movable portion 32 of an adjacent suspension spring 30, lodged in a through hole 43 with a radial gap R inferior to the elastic deformation admitted for the suspension spring 30, in a direction orthogonal to the axis of the motor-compressor assembly 10 and inferior to a radial spacing AR between the motor-compressor assembly 10 and the shell 1.
  • This radial gap R can be variable around the respective mounting element 20, although the constructions illustrated and described below present a constant radial gap R around each mounting element 20.
  • the stop element 40 presents a through hole 43 centrally produced in the free end portion 42 of a respective stop element 40, and which is conformed to entirely surround, with the radial gap R, an extension of the adjacent mounting element 20.
  • one of the stop elements 40 has the respective free end portion 42 provided with a through hole 43, as already described, and which entirely surrounds, with the radial gap R, an extension of the mounting element 20 projecting from an adjacent end of the cylinder block 11.
  • At least one of the stop elements 40 presents its through hole 43 partially surrounding, with the radial gap R, an extension of the mounting element 20, said through hole 43 presenting an open contour and being provided with a radial slot 43a open outwardly from the respective stop element 40, to allow an extension of the adjacent mounting element 20 to be radially fitted in its interior.
  • the stop elements 40 used for mounting the motor-compressor assembly 10 within the shell 1 present different constructions, particularly as to the free end portion 42, one of said constructions having the respective through hole 43 with a closed contour and the other presenting the respective through hole 43 with an open contour and defining a radial slot 43a, as exposed above.
  • the stop elements 40 are resistant to pulling and compression forces and present a certain flexibility in the displacing direction of the piston 14, which is sufficient to absorb part of the impact energy when the adjacent end of the motor-compressor assembly 10 is seated against said piston 14.
  • the free end portions 42 thereof are different from one another, and they are constructed according to mounting requirements of the adjacent end of the cylinder block 11.
  • the through hole 43 is defined so as to entirely surround, with a radial gap, an extension of an adjacent mounting element 20.
  • the mounting element 20 is in the form of a rigid rod 22, of circular cross section, which coaxially traverses a through hole 43, which entirely surrounds and with the radial gap R, said rigid rod 22.
  • the through hole 43 is in the form of a central through hole, with a closed and also circular contour.
  • the mounting of the motor-compressor assembly 10 to this stop element 40 occurs by passing, through a through hole 43 centralized in the respective stop element 40, a mounting element 20, until reaching a central hole 34 of an adjacent suspension spring 30.
  • an end 22a of a rigid rod 22, defining the mounting element 20 can traverse also the central hole 34, receiving a fixation means 50 which retains said rigid rod 22 to said suspension spring 30.
  • the end 22a is also provided with a hole to be aligned with the central hole 34 of the suspension spring 30, in order to receive an extension of the fixation means 50.
  • the suspension system of the present invention For mounting the stop element 40 to the end 10a of the motor-compressor assembly 10 adjacent to the cylinder cover 12, the suspension system of the present invention provides said stop element 40 with its through hole 43 partially surrounding, and with the a radial gap R, an extension of the adjacent mounting element 20, said through hole 43 presenting an open contour and being provided with a radial slot 43a open outwardly from the stop element 40, so as to allow an extension of the adjacent mounting element 20 to be radially fitted in its interior.
  • the mounting element 20 is defined by a rigid rod 21, having a respective free end 21a axially projecting from the cylinder cover 12, said rigid rod 21 and through hole 43 each presenting a respective non-circular cross section, for example, substantially rectangular.
  • the through hole 43 presents a substantially rectangular contour having a vertical width Lv inferior, preferably substantially inferior, to a horizontal length Ch, and the radial slot 43a presents a horizontal width Lh inferior to the horizontal length Ch of the respective through hole 43.
  • the mounting element 20 presents a cross section having a horizontal dimension slightly inferior to the horizontal length Ch of the through hole 43 and superior to the horizontal width Lh of the radial slot 43a and to the vertical width Lv of the through hole 43, said dimensions being defined to allow the mounting element 20 to be radially fitted in the interior of the through hole 43, in a position angularly displaced in relation to a final mounting position, in which said mounting element 20 remains radially retained in the interior of the through hole 43.
  • the mounting element 20 may be also defined by a pair of laterally adjacent rigid rods.
  • the mounting of the motor-compressor assembly 10 in the interior of the shell 1 occurs after attaching, to said shell 1, the stop elements 40 duly positioned therewithin and at least one suspension spring 30 being attached to each stop element. With the stop elements 40 and suspension springs 30 already positioned, the motor-compressor assembly 10 is mounted by disposing, through the through hole 43 of one of the stop elements 40, the rigid rod 22 adjacent to the resonant spring 16, until its end 22a reaches the adjacent suspension spring 30 and is attached thereto.
  • the first stop element 40 to be traversed by a mounting element 20 is the one whose through hole 43 has a closed contour.
  • the motor-compressor assembly 10 is subjected to a small rotation around its longitudinal axis, until the rigid rod 21, which defines the other mounting element 20, is introduced, slightly inclined, through the radial slot 43a of the through hole 43 of the other stop element 40, and reaches the interior of said through hole 43. Then, said rigid rod 21 is conducted to a horizontal position, orthogonal to the longitudinal axis of the adjacent stop element 40, receiving, in this position, fixation means 50, such as screws, for attaching the adjacent suspension spring 30 to the cylinder block 11.
  • fixation means 50 such as screws
  • the through hole 43 thereof presents, in its contour, at least one recess 45, eccentric to its radial slot 43a and which is dimensioned to accommodate a lateral edge of the mounting element 20, during the initial phase in which the latter is radially fitted in the interior of the through hole 43.
  • the recess 45 is produced in an inner wall portion of the through hole 43, as illustrated in figures 9 , 12 and 13 .
  • each stop element 40 has the respective through hole 43 conformed so that the passage of an extension portion of each rigid rod 21, 22, through the respective through hole 43, occurs with a radial gap R which does not provoke any type of interference upon normal operation of the compressor, but which provides displacement limiting means for the motor-compressor assembly 10, at least in the compressor transport and handling situations.
  • the suspension system of the present invention has the advantages of: preventing the motor-compressor assembly 10 from striking the shell 1; preventing the excessive deformation of the springs in the direction orthogonal to the axis of the motor-compressor assembly 10; protecting the suspension springs 30 against break, by avoiding impacts thereof against the shell 1 and also against the stop elements 40.
  • the suspension system of the motor-compressor assembly 10 of the present invention presents the advantage of having low cost and being easy to be manufactured, since the stop elements 40 are in the form of a stamped piece, being affixed by already widely known conventional fixation processes.
  • the present invention is also applicable to the constructions in which, on each side of the motor-compressor assembly 10, is mounted a suspension spring 30 or even a plurality of suspension springs 30, defining a leaf spring assembly.
  • the suspension system of the present invention permits providing a stop element 40 of the type presented herein for each suspension spring 30 of the leaf spring assembly, or also a single stop element 40 for each suspension leaf spring assembly disposed on each side of the motor-compressor assembly 10 and adjacent to a suspension spring 30 provided closer to the motor-compressor assembly 10.
  • Each plurality of suspension springs 30 can have at least part of their suspension springs 30 mounted to the shell 1 directly to the latter or through the stop elements 40 disposed on the same side of the motor-compressor assembly 10, or said suspension springs 30 can be mounted to a common portion, which is then mounted to the stop element 40.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressor (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
EP08783091.5A 2007-05-31 2008-05-30 Suspension system for a linear compressor Active EP2148987B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
BRPI0702461-4A BRPI0702461B1 (pt) 2007-05-31 2007-05-31 Sistema de suspensão para compressor linear
PCT/BR2008/000162 WO2008144872A1 (en) 2007-05-31 2008-05-30 Suspension system for a linear compressor

Publications (2)

Publication Number Publication Date
EP2148987A1 EP2148987A1 (en) 2010-02-03
EP2148987B1 true EP2148987B1 (en) 2018-04-04

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Application Number Title Priority Date Filing Date
EP08783091.5A Active EP2148987B1 (en) 2007-05-31 2008-05-30 Suspension system for a linear compressor

Country Status (9)

Country Link
US (1) US8371827B2 (pt)
EP (1) EP2148987B1 (pt)
JP (1) JP5456662B2 (pt)
KR (1) KR101451953B1 (pt)
CN (1) CN101802403B (pt)
BR (1) BRPI0702461B1 (pt)
ES (1) ES2673631T3 (pt)
TR (1) TR201808567T4 (pt)
WO (1) WO2008144872A1 (pt)

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KR100548446B1 (ko) * 2003-09-22 2006-02-02 엘지전자 주식회사 왕복동식 압축기의 고정장치
KR100529933B1 (ko) * 2004-01-06 2005-11-22 엘지전자 주식회사 리니어 압축기
KR100527176B1 (ko) * 2004-03-09 2005-11-09 삼성광주전자 주식회사 리니어 압축기
CN101052805B (zh) * 2004-11-02 2012-12-26 菲舍尔和佩克尔应用有限公司 用于线性压缩机的悬挂弹簧
US20070020121A1 (en) * 2005-07-21 2007-01-25 Halkyard Crispin R Suspension Element for Linear Compressor
US20070020122A1 (en) * 2005-07-25 2007-01-25 Halkyard Crispin R Suspension for Linear Compressor
DE102005038783A1 (de) * 2005-08-17 2007-02-22 Danfoss Compressors Gmbh Linearverdichter

Also Published As

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EP2148987A1 (en) 2010-02-03
US20100172769A1 (en) 2010-07-08
BRPI0702461B1 (pt) 2018-07-10
KR101451953B1 (ko) 2014-10-16
KR20100019996A (ko) 2010-02-19
US8371827B2 (en) 2013-02-12
JP2010528215A (ja) 2010-08-19
TR201808567T4 (tr) 2018-07-23
CN101802403B (zh) 2012-05-02
CN101802403A (zh) 2010-08-11
ES2673631T3 (es) 2018-06-25
BRPI0702461A2 (pt) 2009-01-20
WO2008144872A1 (en) 2008-12-04
JP5456662B2 (ja) 2014-04-02

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